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1.发明申请PROCESS OF FORMING A MATERIAL HAVING NANO-PARTICLES AND A MATERIAL HAVING NANO-PARTICLES 有权形成具有纳米颗粒的材料的方法和具有纳米颗粒的材料公开(公告)号：US20120171438A1
公开(公告)日：2012-07-05
申请号：US12983421
申请日：2011-01-03
CPC分类号： B81B7/04 , B05D3/20 , B05D3/207 , B05D5/12 , B05D7/24 , B29C70/08 , B29C70/14 , B29C70/88 , B29K2077/10 , B29K2105/124 , B29K2105/167 , B29K2277/10 , B29K2477/10 , B29K2677/10 , B29K2877/10 , B81C1/00 , B82Y30/00 , B82Y40/00 , C08J3/20 , C08J5/005 , Y10T428/24893
摘要： A process of forming a material having nano-particles and a material having nano-particles are disclosed. The process includes arranging nano-particles in a predetermined pattern within a matrix material. The material includes arranged nano-particles forming a predetermined pattern in the matrix material.
摘要翻译： 公开了一种形成具有纳米颗粒的材料和具有纳米颗粒的材料的方法。 该方法包括以矩阵材料中的预定图案布置纳米颗粒。 该材料包括在基体材料中形成预定图案的布置的纳米颗粒。
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公开(公告)号：US07556475B2
公开(公告)日：2009-07-07
申请号：US11443723
申请日：2006-05-31
IPC分类号： F01D11/08
CPC分类号： F01D11/08 , F05D2230/64 , F05D2240/11 , Y10T29/4932
摘要： A method facilitates the assembly of a turbine engine. The method includes providing a shroud support block having a forward end and an aft end, coupling a forward end of a shroud to the shroud support block using a forward fastener, and coupling an aft end of the shroud to the shroud support block using an aft fastener. The method also includes installing a locking pin through the aft fastener to retain the aft fastener, and staking the locking pin in the shroud support block, such that the locking pin is securely coupled to the shroud support block.
摘要翻译： 一种方法有助于涡轮发动机的组装。 该方法包括提供具有前端和后端的护罩支撑块，使用前向紧固件将护罩的前端连接到护罩支撑块，并且使用后部将护罩的后端连接到护罩支撑块 紧固件。 该方法还包括通过后部紧固件安装锁定销以保持后部紧固件，并将锁定销钉固定在护罩支撑块中，使得锁定销牢固地联接到护罩支撑块。
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3.发明申请TURBOMACHINE COMPONENT HAVING AN INTERNAL CAVITY REACTIVITY NEUTRALIZER AND METHOD OF FORMING THE SAME 有权具有内部孔反应性中和剂的涡轮分量及其形成方法公开(公告)号：US20130291513A1
公开(公告)日：2013-11-07
申请号：US13464134
申请日：2012-05-04
CPC分类号： F01D5/18 , F01D5/147 , F01D5/282 , F01D5/284 , F01D5/286 , F01D5/288 , F05D2300/224 , F05D2300/2261 , Y10T29/49231
摘要： A turbomachine component includes a body having an exterior surface and an interior surface, an internal cavity defined by the interior surface, and a reactivity neutralizing member arranged within the internal cavity. The reactivity neutralizing member is configured and disposed to neutralize turbomachine combustion products on the interior surface of the body.
摘要翻译： 涡轮机组件包括具有外表面和内表面的本体，由内表面限定的内腔，以及布置在内腔内的反应性中和构件。 反应性中和构件被构造和设置成中和体内内表面上的涡轮机燃烧产物。
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4.发明申请Continuous Fiber Reinforced Mesh Bond Coat for Environmental Barrier Coating System 有权用于环境屏障涂层系统的连续纤维增强网状粘结涂层公开(公告)号：US20130177440A1
公开(公告)日：2013-07-11
申请号：US13348212
申请日：2012-01-11
CPC分类号： F01D5/288 , C04B41/009 , C04B41/52 , C04B41/89 , F05D2230/90 , F05D2300/20 , F05D2300/6034 , F05D2300/614 , Y02T50/672 , C04B35/80 , C04B41/5096 , C04B14/46 , C04B41/4501 , C04B41/5024
摘要： A gas turbine blade may have a bond coat applied to its surface. A porous substrate may be applied to the bond layer and one or more protective layers may be applied to the bond layer such that the fiber mesh is embedded between the bond layer and the protective layer to prevent creep.
摘要翻译： 燃气轮机叶片可以具有施加到其表面的粘合涂层。 可以将多孔基材施加到接合层，并且可以将一个或多个保护层施加到接合层，使得纤维网嵌入在接合层和保护层之间以防止蠕变。
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5.发明申请公开(公告)号：US20130022471A1
公开(公告)日：2013-01-24
申请号：US13188755
申请日：2011-07-22
申请人： Herbert Chidsey Roberts, III , Paul Edward Gray , Roger Lee Ken Matsumoto , Jeffrey H. Boy , Philip Harold Monaghan , Joseph Halada
发明人： Herbert Chidsey Roberts, III , Paul Edward Gray , Roger Lee Ken Matsumoto , Jeffrey H. Boy , Philip Harold Monaghan , Joseph Halada
CPC分类号： F01D5/005 , C04B41/009 , C04B41/52 , C04B41/89 , F01D5/147 , F01D5/282 , F01D5/284 , F05D2300/6033 , Y10T29/49318 , C04B35/80 , C04B41/4539 , C04B41/4572 , C04B41/4582 , C04B41/5025 , C04B14/4693 , C04B41/5059 , C04B41/522 , C04B41/4523
摘要： Methods for repairing a turbine airfoil constructed from a CMC material are provided via filling a cavity located in the turbine airfoil with a ceramic paste (e.g., including a ceramic powder and a binder), heating the ceramic paste in the cavity to remove the binder, thereby forming a porous ceramic material, and adding a molten ceramic material to the porous ceramic material. The cavity can be defined in an airfoil of the turbine airfoil (e.g., on a tip or cap of the airfoil). Intermediates formed during the repair of a turbine airfoil are also provided. The intermediate can generally include an airfoil comprising a CMC material, a cavity defined in the airfoil, and a porous ceramic material filling the cavity.
摘要翻译： 通过用陶瓷浆（例如，包括陶瓷粉末和粘合剂）填充位于涡轮机翼型中的空腔来提供用于修复由CMC材料构成的涡轮机翼型的方法，加热腔中的陶瓷浆料以除去粘合剂， 从而形成多孔陶瓷材料，并将熔融陶瓷材料加入到多孔陶瓷材料中。 空腔可以限定在涡轮机翼型的翼型（例如，在翼型的尖端或盖上）。 还提供在涡轮翼型修复期间形成的中间体。 中间体通常可以包括包含CMC材料的翼型，在翼型中限定的空腔和填充空腔的多孔陶瓷材料。
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公开(公告)号：US08333340B2
公开(公告)日：2012-12-18
申请号：US13007697
申请日：2011-01-17
CPC分类号： B29C70/887 , B29C53/32 , B32B2305/08
摘要： A system for reinforcing a substrate includes a rotary device, a first guide connected to the rotary device, and a form positioned against the first guide. A reinforcement is supplied to wind around the form and against the first guide. A method for reinforcing a substrate includes connecting a first guide to a rotary device and positioning a form on a first side of the first guide. The method further includes winding a reinforcement around the form and against the first side of the first guide.
摘要翻译： 用于加强基板的系统包括旋转装置，连接到旋转装置的第一引导件和抵靠第一引导件定位的形式。 供应钢筋以围绕形式缠绕在第一导轨上。 一种用于加强基板的方法包括将第一引导件连接到旋转装置并将形式定位在第一引导件的第一侧上。 所述方法还包括围绕所述形式缠绕加强件并抵靠所述第一导向件的第一侧。
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7.发明授权Turbomachine component having an internal cavity reactivity neutralizer and method of forming the same 有权具有内腔反应性中和剂的涡轮机组分及其形成方法公开(公告)号：US09587492B2
公开(公告)日：2017-03-07
申请号：US13464134
申请日：2012-05-04
CPC分类号： F01D5/18 , F01D5/147 , F01D5/282 , F01D5/284 , F01D5/286 , F01D5/288 , F05D2300/224 , F05D2300/2261 , Y10T29/49231
摘要： A turbomachine component includes a body having an exterior surface and an interior surface, an internal cavity defined by the interior surface, and a reactivity neutralizing member arranged within the internal cavity. The reactivity neutralizing member is configured and disposed to neutralize turbomachine combustion products on the interior surface of the body.
摘要翻译： 涡轮机组件包括具有外表面和内表面的本体，由内表面限定的内腔，以及布置在内腔内的反应性中和构件。 反应性中和构件被构造和设置成中和体内内表面上的涡轮机燃烧产物。
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公开(公告)号：US08956700B2
公开(公告)日：2015-02-17
申请号：US13276713
申请日：2011-10-19
CPC分类号： C23C4/02 , B05D3/102 , F01D5/14 , F01D5/288 , F05D2230/90 , Y10T428/24777
摘要： A method for adhering a coating to a substrate structure comprises selecting a substrate structure having an outer surface oriented substantially parallel to a direction of radial stress, modifying the outer surface to provide a textured region having steps to adhere a coating thereto, and applying a coating to extend over at least a portion of the textured region, wherein the steps are oriented substantially perpendicular to the direction of radial stress to resist deformation of the coating relative to the substrate structure. A rotating component comprises a substrate structure having an outer surface oriented substantially parallel to a direction of radial stress. The outer surface defines a textured region having steps to adhere a coating thereto, and a coating extends over at least a portion of the textured region. The steps are oriented substantially perpendicular to the direction of radial stress to resist creep.
摘要翻译： 用于将涂层粘附到基底结构的方法包括选择具有基本上平行于径向应力的方向定向的外表面的基底结构，改变外表面以提供具有将涂层附着到其上的步骤的纹理区域，以及施加涂层 以延伸至纹理区域的至少一部分，其中所述台阶基本垂直于径向应力的方向定向，以抵抗涂层相对于基底结构的变形。 旋转部件包括具有基本上平行于径向应力的方向定向的外表面的基底结构。 外表面限定具有将涂层粘附到其上的步骤的纹理区域，并且涂层在纹理化区域的至少一部分上延伸。 这些台阶基本上垂直于径向应力的方向定向以抵抗蠕变。
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9.发明授权Process of forming a material having nano-particles and a material having nano-particles 有权形成具有纳米颗粒的材料和具有纳米颗粒的材料的方法公开(公告)号：US08945688B2
公开(公告)日：2015-02-03
申请号：US12983421
申请日：2011-01-03
CPC分类号： B81B7/04 , B05D3/20 , B05D3/207 , B05D5/12 , B05D7/24 , B29C70/08 , B29C70/14 , B29C70/88 , B29K2077/10 , B29K2105/124 , B29K2105/167 , B29K2277/10 , B29K2477/10 , B29K2677/10 , B29K2877/10 , B81C1/00 , B82Y30/00 , B82Y40/00 , C08J3/20 , C08J5/005 , Y10T428/24893
摘要： A process of forming a material having nano-particles and a material having nano-particles are disclosed. The process includes arranging nano-particles in a predetermined pattern within a matrix material. The material includes arranged nano-particles forming a predetermined pattern in the matrix material.
摘要翻译： 公开了一种形成具有纳米颗粒的材料和具有纳米颗粒的材料的方法。 该方法包括以矩阵材料中的预定图案布置纳米颗粒。 该材料包括在基体材料中形成预定图案的布置的纳米颗粒。
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10.发明申请FIBER-REINFORCED BARRIER COATING, METHOD OF APPLYING BARRIER COATING TO COMPONENT AND TURBOMACHINERY COMPONENT 审中-公开纤维增强型遮蔽涂层，将遮蔽涂层应用于组件和涡轮机组件的方法公开(公告)号：US20130260130A1
公开(公告)日：2013-10-03
申请号：US13435434
申请日：2012-03-30
IPC分类号： B32B5/02 , B05D1/08 , C23C4/18 , B32B9/04 , B32B27/02 , B32B15/02 , B32B17/02 , C08K3/34 , C08K3/04 , C08K3/08 , C08K3/02 , C08K3/38 , C09D177/10 , C08K3/40 , B05D3/02
CPC分类号： C23C28/321 , C04B41/009 , C04B41/52 , C04B41/89 , C23C24/08 , C23C28/3215 , C23C28/322 , C23C28/34 , C23C28/341 , C23C28/345 , C23C28/3455 , C23C28/42 , F01D5/288 , F05D2300/2261 , F05D2300/603 , F05D2300/614 , Y10T428/249924 , Y10T428/26 , Y10T428/31678 , Y10T428/31725 , C04B35/565 , C04B35/806 , C04B35/584 , C04B41/5096 , C04B41/5059 , C04B41/522 , C04B41/5024 , C04B41/5037 , C04B41/4539 , C04B41/4596 , C04B41/5042
摘要： A method of applying a barrier coating to a component is provided. The method includes providing the component and preparing a slurry comprising a mixture. The mixture includes about 50-90 percent by volume fraction of a barrier coating composition, the barrier coating composition and 10-50 percent by volume fraction of a plurality of short fibers. The method includes applying at least one layer of the slurry to at least a portion of the component and curing the slurry on the portion of the component to obtain a fiber-reinforced barrier coating.
摘要翻译： 提供了向部件施加阻挡涂层的方法。 该方法包括提供组分并制备包含混合物的浆料。 该混合物包括约50-90％（体积）的阻隔涂料组合物，阻隔涂料组合物和10-50％（体积）分数的多种短纤维。 该方法包括将至少一层浆料施加到部件的至少一部分上并固化部件部分上的浆料以获得纤维增强的阻挡涂层。
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